The results obtained in setting up a theory of stability of fibrous and laminated composites in the case where the plane Π is in an arbitrary position are analyzed. The plane Π is formed by the points of a buckling mode that have equal phases relative to the line of compression. This theory follows from the linearized three-dimensional theory of stability of deformable bodies and is used to determine the critical compressive load and the associated position of the plane Π. Numerical examples are presented. A brief historical sketch is given
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Translated from Prikladnaya Mekhanika, Vol. 45, No. 6, pp. 4–41, June 2009.
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Guz, A.N. Setting up a theory of stability of fibrous and laminated composites. Int Appl Mech 45, 587–612 (2009). https://doi.org/10.1007/s10778-009-0216-5
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DOI: https://doi.org/10.1007/s10778-009-0216-5